NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Model support roll balance and roll couplingThe design concepts of two specialized wind tunnel model support mechanisms are described. The forced oscillation roll balance mechanism was designed to meet the specific requirement to measure aerodynamic forces and moments to permit determination of the damping-in-roll parameters of winged configurations. A variable speed motor is used to oscillate the model by means of an offset crank. The oscillating motion is resisted by a torsion spring to provide a restoring torque and is attached to the section forward of the strain-gage balance. This spring action allows the model to be oscillated at a frequency for velocity resonance, whereby the mechanical spring and any aerodynamic spring balance. This spring action allows the model to be oscillated at a frequency for velocity resonance, whereby the mechanical spring and any aerodynamic spring balance out the model inertia. The only torque then required to oscillate the model at that particular frequency is equal to that due to aerodynamic damping. The second mechanism, a roll coupling for remotely rotating a model, was designed to invert or roll a model about its longitudinal axis when mounted for testing.
Document ID
19740003568
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sharpes, R. E.
(NASA Langley Research Center Hampton, VA, United States)
Carroll, W. J.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Publication Information
Publication: The 8th Aerospace Mech. Symp. te
Subject Category
Facilities, Research, And Support
Accession Number
74N11681
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available